FIELD: weapons and ammunition.
SUBSTANCE: control signals are generated with the help of two identical control channels, in every of which the following control signals are generated for one of missile aerodynamic control surfaces pairs - control signal with feedback on angular speed, control signal with feedback on side linear acceleration and control signal with feedback on missile attack angle. At the same time signal of error proportional to difference of radio control signal and signal, which is proportional to value of side linear acceleration, are integrated, which provides for absence of offset in closed stabilisation system. The novelty is calculation of missile attack angle and generation of according signal, as a result of which positional feedback is provided by angle of missile attack, and missile control accuracy is improved.
EFFECT: improved accuracy of control.
3 cl, 3 dwg
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Authors
Dates
2009-11-27—Published
2007-12-05—Filed